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Azimuthal Spoke Propagation in Hall Effect ThrustersSpokes are azimuthally propagating perturbations in the plasma discharge of Hall Effect Thrusters (HETs) that travel in the E x B direction and have been observed in many different systems. The propagation of azimuthal spokes are investigated in a 6 kW HET known as the H6 using ultra-fast imaging and azimuthally spaced probes. A spoke surface is a 2-D plot of azimuthal light intensity evolution over time calculated from 87,500 frames/s videos. The spoke velocity has been determined using three methods with similar results: manual fitting of diagonal lines on the spoke surface, linear cross-correlation between azimuthal locations and an approximated dispersion relation. The spoke velocity for three discharge voltages (300, 400 and 450 V) and three anode mass flow rates (14.7, 19.5 and 25.2 mg/s) yielded spoke velocities between 1500 and 2200 m/s across a range of normalized magnetic field settings. The spoke velocity was inversely dependent on magnetic field strength for low B-field settings and asymptoted at B-field higher values. The velocities and frequencies are compared to standard drifts and plasma waves such as E x B drift, electrostatic ion cyclotron, magnetosonic and various drift waves. The empirically approximated dispersion relation yielded a characteristic velocity that matched the ion acoustic speed for 5 eV electrons that exist in the near-anode and near-field plume regions of the discharge channel based on internal measurements. Thruster performance has been linked to operating mode where thrust-to-power is maximized when azimuthal spokes are present so investigating the underlying mechanism of spokes will benefit thruster operation.
Document ID
20150008029
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Sekerak, Michael J.
(Michigan Univ. Ann Arbor, MI, United States)
Longmier, Benjamin W.
(Michigan Univ. Ann Arbor, MI, United States)
Gallimore, Alec D.
(Michigan Univ. Ann Arbor, MI, United States)
Brown, Daniel L.
(Air Force Research Lab. Edwards AFB, CA, United States)
Hofer, Richard R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Polk, James E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 12, 2015
Publication Date
October 6, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IEPC-2013-143
Meeting Information
Meeting: IEPC 2013 - International Electric Propulsion Conference
Location: Washington, DC
Country: United States
Start Date: October 6, 2013
End Date: October 10, 2013
Sponsors: George Washington Univ.
Distribution Limits
Public
Copyright
Other
Keywords
Cylindrical Hall Thruster (CHT)
discharge current

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